1、 INCH-POUND MIL-PRF-32271/10A 26 MAY 2010 Superseding MIL-PRF-32271/10 30 October 2008 PERFORMANCE SPECIFICATION SHEET BATTERY, NON-RECHARGEABLE, LITHIUM This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the product he
2、rein shall consist of this specification sheet and MIL-PRF-32271. See NOTES for nominal dimensions; see applicable drawing for dimensional requirements. FIGURE 1 General view, M32271/10 battery shape REFERENCES NAVAIR 1794AS053 Performance Specification for Batteries, Non-Rechargeable, High Performa
3、nce (LIMNO2) (Copies of this document are available from Naval Air Systems Command, Patuxent River, MD 20670-1547) REQUIREMENTS (see 1.2 for Type, Class, and Features descriptions): Type I Class 2 Features D PIN M32271/10-12D Approved chemistry: Lithium manganese dioxide (Li/MnO2) AMSC N/A FSC 6135
4、DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited Copyright Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32271/10A Specification requirements: The
5、following requirements of MIL-PRF-32271, identified therein by Requirement Specification Reference Applicabilitythe phrase “when specified”, are applicable as indicated below: e d vice tput shor ircuit 3tion RT .7.8 marking marking 3.8.5 Yes imensions, marking and configurationParallel cell arrangem
6、ents13.4 Yes Connectors23.4.5 Yes Battery charger connection 3.4.5.1 No Connection integrity 3.4.5.2 YesTerminal integrity 3.4.6 No Complete discharg e 3.4.7 YesState of charge device 3.4.8 Yes State of charge data ou 3.4.8e No Cell charging 3.5.3 YesNail penetration 3.5.4 Yes Cell series string t c
7、 3.5.6 Yes Parallel string charge protection 3.5.6.1 Yes Charge protection 3.5.11 Yes Over-current protection 3.5.13.1 Yes Over-temperature protec 3.5.14 Yes Surface temperature 3.6h Yes Capacity tests LR and L No Immersion 3 No Watertight integrity 3.7.9 Yes DO NOT CHARGE! 3.8.1.2b No Complete disc
8、harge device 3.8.4 Yesmarking/label State of chargeD Battery Drawing A3315887 .1.7) Drawing A3315887 1 attery voltages (3.4.4 7.5 volts for t voltage test Minimum 8.0 volts ell closed circuit voltage test (3.4.4.3 4.6.1.7.2; insertion and withdrawal measurements not required for this battery 3 Copyr
9、ight Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32271/10A est Requirement Specification Reference ApplicabilityT d vice shorection tectiotion ell closed-circuit voltage testCom
10、plete discharge e 4.6.1.9 Yes State of charge device 4.6.1.10 Yes Cell charging 4.6.2.3 Yes Nail penetration 4.6.2.4 Yes Cell series string t 4.6.2.6 Yes Parallel cell charge prot54.6.2.6.1 Yes Charge protection test 4.6.2.11 Yes Battery over-current pro n 4.6.2.13 Yes Battery over-temperature prote
11、c 4.6.2.14 Yes Surface temperature 4.6.4.1 Yes Capacity test LR 4.6.4.1.5 No Capacity test LRT 4.6.4.1.9 No Immersion 4.6.5.8 No Watertight integrity 4.6.5.9 Yes C : When cells are tested as specified in 4.6.1.3, load each cell to be , ell attery closed-circuit voltage testused in a single series ce
12、ll string design with 1 ampere constant current, 2 ohms constant resistance, or 2 watts constant power. In the event that parallel cell arrangements are useduse a load that produces a current equivalent to 1 ampere divided by the number of parallel cstrings to be used, as a minimum. B : When tested
13、as specified in 4.6.1.5.2, load the battery with 1 imensions (4.6.1.6)ampere constant current, 8 ohms constant resistance, or 8 watts constant power. D . Reference Drawing A3315887. Dimension D6 shall be measured in not tatic connection integrity (4.6.1.7.2)less than two places: at the top (terminal
14、 end) and bottom of the battery. The same tolerance shall apply in both locations. S : Connect batteries subjected to this test to test fixture, ynamic connection integrity (4.6.1.7.3)General Dynamics P/N 01-P49797J001. Center applied weight at a location 2.00 0.125 inches from the terminal end of t
15、he battery. D . Connect batteries subjected to this test to test fixture, buse test, pre-dischargeGeneral Dynamics P/N 01-P49797J001. A : When tested as specified in 4.6.2.12a, discharge with a load of either buse test, pulse discharge1 ampere or 12 watts for 1.6 hours. A : When tested as specified
16、in 4.6.2.12i, discharge with a load of 1.25 attery over-current protectionamperes for 1 minute followed by 1.1 amperes for 4 minutes, cycled continuously to 7.5 volts. B : When tested as specified in 4.6.2.13, load batteries with either 3.75 amperes or 45 watts. 5This test only required if parallel
17、cell arrangements are used 4 Copyright Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32271/10A Capacity tests (4.6.4): Test Discharge Rate Duty Cycle I See Below Continuous discha
18、rge to cut-off volts, followed by 650 milli-amperes to zero volts, then 650 milli-amperes forced discharge for 5 minutes L See Below Continuous discharge to cut-off voltage H See Below Continuous discharge to cut-off voltage H2 See Below Continuous discharge to cut-off voltage IT See Below Continuou
19、s discharge to cut-off voltage LT See Below Continuous discharge to cut-off voltage HT See Below Continuous discharge to cut-off voltage Discharge Rate for all capacity tests except H2 (4.6.4): Discharge continuously at 1.8W for 267 seconds, followed by 7.2W for 30 seconds, followed by 26W for 3 sec
20、onds, to cut-off volts. Discharge Rate for H2 capacity test (4.6.5.9e): Discharge continuously at 8.5 watts for 2.1 seconds followed by 3.0 watts for 18.9 seconds to cut-off volts. Watertight integrity (4.6.5.9): Connect batteries subjected to this test to a connector consisting of General Dynamics
21、P/Ns 64-P21451J001 (coupler plate, 1 each), 84-P21427J001 (PWB, 1 each), and 39-P21428J001 (contact, 2 each), whenever connection to a test fixture is required by 4.6.5.9. When assembled, insure that this fixture forms an air-tight seal against the battery. Parts and materials in addition to those s
22、pecified are permissible in order to obtain the air-tight seal provided they do not extend below the contact surface of the battery. VARIANCES: Each battery shall comply with MIL-PRF-32271 except as follows: Add the following paragraphs: 3.4.11 Magnet. Each battery shall include a magnet conforming
23、to 3.1.1, 3.1.8, and Figure 2 of NAVAIR 1794AS0953 for purposes of identifying its rate capability to HOOK-112 radios. When tested as specified in 4.6.1.11, the magnet shall have not less than 15 ampere-turns of magnetomotive force. 4.6.1.11 Magnet test. Each battery shall be tested for magnetomotiv
24、e force within the volume specified by Figure 2 of NAVAIR 1794AS0953. Modify tables as follows: TABLE III Group III Battery Inspections and Tests. Add the following after “Connector” Group No. Sample Size Inspection Requirement Paragraph Test Method Paragraph III 23 Magnet test 3.4.11 4.6.1.11 5 Cop
25、yright Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32271/10A Table IX Group B Inspections and Tests. Add the following after “Charge protection” Inspection or Test Requirement P
26、aragraph Method or Test Paragraph Test sample break-out by test Magnet test 1/ 3.4.11 4.6.1.11 All NOTES: (This section contains information of a general nature which may be helpful, but is not mandatory) Intended use: This battery is intended to operate the family of AN/PRC-112 survival radios as w
27、ell as their companion program loaders. It can also be used to power a training device for Wide Area Munitions. 6Nominal ratings: The following are the nominal ratings for each battery type described by this specification sheet. They are provided for information purposes. Battery PIN: M32271/10-12D
28、(Li/MnO2) Overall Dimensions: 3.31 in H x 2.25 in W x 1.54 in D MAX Weight: 0.6 lbs (272 grams) Voltage Range: 7.5 13.20 Nominal Capacity:(in ampere-hours) 3.25 Amp-hrs Nominal Energy:(in watt-hours) 39 Watt-hrs MAX rated power output: 26 watts (3s pulse) MAX continuous load rating: 1.0 ampere MAX p
29、ulse load rating: 3.5 amperes Instantaneous trip rating: 4.0 amperes Operating temperature range: -40 to 130F (-40 to 55C) Storage temperature range: -40 to 160F (-40 to 71C) MAX abusive temperature: (non-operating) 195F (91C) Other data: Military Type Designations. The military type designation tha
30、t relates to the PIN covered by this specification sheet is as follows: The BA-5312()/U designation has been used for the Type I PIN. It should be noted that the Type II BA-5112()/U has been replaced by the BA-5312()/U. This battery is subject to the transportation requirements of 49 CFR 173.185. Th
31、e battery has solid cathodes and more than 2.0 grams of lithium content. See applicable Material Safety Data Sheet (MSDS) for the maximum lithium weight per cell and battery. It should be noted that all non-rechargeable lithium batteries are restricted from shipment as cargo aboard passenger aircraf
32、t within, entering, or leaving the US. 6Capacity and energy delivered by a battery are significantly affected by usage conditions, such as temperature and loads applied. If you have any questions about use of this battery in a particular device or circumstance, please visit the following web site (c
33、ontact info is posted): http:/www.cerdec.army.mil/c2d/armypower. 6 Copyright Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32271/10A 7 This battery includes a complete discharge d
34、evice in order to render the battery as non-reactive after use. If the battery is damaged, or if the device does not operate as indicated by an amber or yellow light, the battery is considered reactive waste. This battery may be recycled after use. Universal waste rules, where applicable, apply only
35、 when recycling is the chosen disposal method. Navy safety tests of NAVSEA S9310-AQ-SAF-010 are required for this battery during first article testing. The test data provided from the testing will be used to evaluate applications for specific using devices and Navy platforms. Devices using this batt
36、ery will require US Navy Safety Approval prior to use by Department of Navy users unless such approval has already been granted. Please consult with NAVSEA Instruction 9310.1 for further information. Changes from previous issue. The margins of this specification are marked with vertical lines to ind
37、icate where changes from the previous issue were made. This was done as a convenience only and the Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irres
38、pective of the marginal notations and relationship to the last previous issue. Custodians: Preparing activity: Army CR Army CR Navy SH (Project Number 6135-2010-034) Air Force 99 DLA CC Review activities: Navy AS, MC Air Force 71 NOTE: The activities listed above were interested in this document as
39、of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at https:/assist.daps.dla.mil or https:/assist.daps.dla.mil/quicksearch/. Copyright Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
